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Description
| - Numerical model of airfoil segment with piezoelectric sensors was created in commercial finite element software Abaqus and its response to impact loading was compared with experimental results. The wing segment is made of woven glass epoxy composite with varying number of plies and type of weave. The material properties were experimentally determined from tensile tests and used in finite element model of rectangular plate. Results from experimental modal analysis of composite rectangular plate made of the same material as the segment were compared to results from numerical analysis and parameters of numerical model were adjusted. Finally, numerical model of whole segment was created and validated on results from corresponding experimental modal analysis. Moreover, piezoelectric sensors were glued to the segment and their response to dynamic loading was compared to results from numerical simulation.
- Numerical model of airfoil segment with piezoelectric sensors was created in commercial finite element software Abaqus and its response to impact loading was compared with experimental results. The wing segment is made of woven glass epoxy composite with varying number of plies and type of weave. The material properties were experimentally determined from tensile tests and used in finite element model of rectangular plate. Results from experimental modal analysis of composite rectangular plate made of the same material as the segment were compared to results from numerical analysis and parameters of numerical model were adjusted. Finally, numerical model of whole segment was created and validated on results from corresponding experimental modal analysis. Moreover, piezoelectric sensors were glued to the segment and their response to dynamic loading was compared to results from numerical simulation. (en)
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Title
| - Numerical model of composite airfoil segment with piezoletric sensors
- Numerical model of composite airfoil segment with piezoletric sensors (en)
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skos:prefLabel
| - Numerical model of composite airfoil segment with piezoletric sensors
- Numerical model of composite airfoil segment with piezoletric sensors (en)
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skos:notation
| - RIV/49777513:23520/14:43924012!RIV15-GA0-23520___
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http://linked.open...avai/riv/aktivita
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http://linked.open...avai/riv/aktivity
| - P(ED1.1.00/02.0090), P(GAP101/11/0288)
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http://linked.open...iv/cisloPeriodika
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http://linked.open...vai/riv/dodaniDat
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http://linked.open...aciTvurceVysledku
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http://linked.open.../riv/druhVysledku
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http://linked.open...iv/duvernostUdaju
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http://linked.open...titaPredkladatele
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http://linked.open...dnocenehoVysledku
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http://linked.open...ai/riv/idVysledku
| - RIV/49777513:23520/14:43924012
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - Glass-epoxy textile composite, Piezoelectricity, Finite element analysis, Modal analysis (en)
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http://linked.open.../riv/klicoveSlovo
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http://linked.open...odStatuVydavatele
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http://linked.open...ontrolniKodProRIV
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http://linked.open...i/riv/nazevZdroje
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http://linked.open...in/vavai/riv/obor
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http://linked.open...ichTvurcuVysledku
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http://linked.open...cetTvurcuVysledku
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http://linked.open...vavai/riv/projekt
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http://linked.open...UplatneniVysledku
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http://linked.open...v/svazekPeriodika
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http://linked.open...iv/tvurceVysledku
| - Bartošek, Jan
- Kroupa, Tomáš
- Smolík, Luboš
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issn
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number of pages
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http://localhost/t...ganizacniJednotka
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